What was found
LWR FUSELAGE PANEL 191QL HAS IMPACT DAMAGE AT AFT END ~ 1" LONG. CLEANED UP DAMAGED AREA POTTED AND APPLIED FIBER GLASS OVERLAY AS PER SRM 51-40-09 AND RESTORED FINISH AS PER MM 51-24-11 IAW EO#4753A796.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LWR FUSELAGE PANEL 191QL HAS IMPACT DAMAGE AT AFT END ~ 1" LONG. CLEANED UP DAMAGED AREA POTTED AND APPLIED FIBER GLASS OVERLAY AS PER SRM 51-40-09 AND RESTORED FINISH AS PER MM 51-24-11 IAW EO#4753A796.